This page no longer updated from 31 October 2001. Latest version can be found at Soyuz ST-2

Gross Mass: 25,200 kg. Empty Mass: 2,355 kg. Thrust (vac): 30,000 kgf. Isp: 359 sec. Burn time: 300 sec. Propellants: Lox/Kerosene Diameter: 2.7 m. Span: 2.7 m. Length: 6.7 m. Country: Russia. No Engines: 1. RD-0124 Status: Development.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .